Zobrazeno 1 - 10
of 86
pro vyhledávání: '"Dario Giuseppe Pastrone"'
Publikováno v:
Journal of Spacecraft and Rockets. 58:1893-1903
In this paper, design and optimization approaches are applied to a hybrid-powered small-satellite launcher, namely a deterministic and a robust-based method. A unique hybrid rocket engine is consid...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6ddb37e9142f2a21e6409e216224f28b
https://doi.org/10.2514/1.a35007
https://doi.org/10.2514/1.a35007
Publikováno v:
Aerospace, Vol 8, Iss 226, p 226 (2021)
Optimization of Hybrid Rocket Engines at Politecnico di Torino began in the 1990s. A comprehensive review of the related research activities carried out in the last three decades is here presented. After a brief introduction that retraces driving mot
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cdd6ed9ef77d24f07ba4068ecc3b8725
https://www.mdpi.com/2226-4310/8/8/226
https://www.mdpi.com/2226-4310/8/8/226
Autor:
Andrea Ferrero, Francesco Nasuti, Antonietta Conte, Emanuele Martelli, Dario Giuseppe Pastrone
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
The dual-bell nozzle is a promising altitude adaptive nozzle concept for improving the performance of existing space launchers as well as future reusable launch vehicles. It is characterized by an inflection in the wall geometry which links a base no
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::10d6f43975698d05735fdf730b25b7bb
https://doi.org/10.2514/6.2021-3586
https://doi.org/10.2514/6.2021-3586
The established state-of-the-art for composite solid propellant grain manufacture consists in mix-cast-cure process using hazardous chemicals and specific molds for propellant forming. In most of the cases, polyaddition of oligomers involves isocyana
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c183d96d4b8262fb983bc550c41e9beb
http://hdl.handle.net/11583/2871025
http://hdl.handle.net/11583/2871025
The application of dual-bell nozzles to existing space launchers offers the possibility to significantly increase their payload capability. This benefit is related to the ability of this kind of nozzles to switch between a low-altitude and a high-alt
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::47910d21078b42accdc135cfe4aa3783
http://hdl.handle.net/11573/1543577
http://hdl.handle.net/11573/1543577
A low-order model for a hybrid rocket engine is proposed to investigate low-frequency combustion instabilities. The present work is based on a one-way coupling between a one-dimensional thermal model to evaluate the unsteady regression rate and a zer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8b470feb0bf431960335c7df61e3c567
http://hdl.handle.net/11583/2782254
http://hdl.handle.net/11583/2782254
The work reported herein is a preliminary numerical study of a resonant igniter for rocket engines. Resonant igniters are very attractive and promising for in-space thrusters, since they are simple, highly reliable and lightweight. Fine-tuning of var
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::008755de16cb865e9fe2314e264647b3
http://hdl.handle.net/11583/2782256
http://hdl.handle.net/11583/2782256
Publikováno v:
Journal of Propulsion and Power. 34:133-145
A novel internal ballistics technique for determining the time-resolved spatially averaged regression rate of the solid-fuel grain in a hybrid rocket engine is presented. This technique makes use o...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b9498221ab2bc0eea54a06fdb87e9d49
https://doi.org/10.2514/1.b36517
https://doi.org/10.2514/1.b36517